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Government Designation: 11D430. Designer: Melnikov. Application: Yantar-2K orbital propulsion. Propellants: N2O4/UDMH. Thrust(vac): 29.430 kN (6,616 lbf). Isp: 307 sec. Burn time: 600 sec. Chambers: 1. Chamber Pressure: 9.00 bar. Country: Russia. Status: In Production. Orbital propulsion system of the Yantar-2K military satellite, including one 11D430, four 11D431, four 11D446, and eight 11D428. Up to 50 ignitions.
11D430 used on Spacecraft
Bibliography and Further Reading - Sorokin, Vladislav, Novosti Kosmonavtiki, "'Yantarnaya istoriya'", 1997, Issue 17, page 57.
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